学者信息
已发表成果：
WOK 论文 9 篇;中文核心 6 篇;其它论文 3 篇;
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Conceptual design methodology and performance evaluation of turbine-based combined cycle inward-turning inlet with twin-design points
Aerospace Science and Technology,1270-9638,2024-09.
Hu, Zhancang; Li, Zhonglong; Tang, Yiqi; Yu, Yaokun; Zhang, Yuchao; Zheng, Xiaogang; Zhu, Chengxian...
WOS:001282525200001 EI:20242716598795 10.1016/j.ast.2024.109309
收录情况：SCIE、EI -
Conceptual Design Methodology and Performance Evaluation of Inward-Turning Tbcc Inlet with Twin-Design Points
SSRN,1556-5068,2024-02-15.
Hu, Zhancang (1); Li, Zhonglong (2); Tang, Yiqi (1); Yu, Yaokun (1); Zhang, Yuchao (2); Zheng, Xiao...
EI:20240080267 10.2139/ssrn.4727097
收录情况：EI -
Stream-Surface Iteration-Based Flowfield Calculation Method for Pressure-Controllable Waverider Design
AIAA JOURNAL,0001-1452,2024-02-07.
Sun, Weiqiang; Zheng, Xiaogang; You, Yancheng
WOS:001157278500001 10.2514/1.J063430
收录情况：SCIE -
Analytical model for curved-shock Mach reflection
Physics of Fluids,1070-6631,2023-03.
Shi, Chongguang; You, Yancheng; Zheng, Xiaogang; Zhu, Chengxiang
WOS:000942071400003 EI:20231013681233 10.1063/5.0139784
收录情况：SCIE、EI -
Analytical model for predicting the length scale of shock/boundary layer interaction with curvature (vol 34, 111701, 2022)
Physics of Fluids,1070-6631,2023-03.
Cheng, Jianrui; Yang, Kai; Zheng, Xiaogang; Shi, Chongguang; Zhu, Chengxiang; You, Yancheng
WOS:000944031400002 EI:20231113740412 10.1063/5.0147923
收录情况：SCIE、EI -
Analytical model for predicting the length scale of shock/boundary layer interaction with curvature
Physics of Fluids,1070-6631,2022-11-01.
Cheng, Jianrui; Yang, Kai; Zheng, Xiaogang; Shi, Chongguang; Zhu, Chengxiang; You, Yancheng
WOS:000890878500029 EI:20225013226437 10.1063/5.0125439
收录情况：SCIE、EI -
Inverse Design of Hypersonic Waveriders with Variable Cross-Section Shock Waves
JOURNAL OF SPACECRAFT AND ROCKETS,0022-4650,2022-11.
Wang, Xiao; Zheng, Xiaogang; Zhu, Chengxiang; You, Yancheng
WOS:000912119400001 EI:20230513461397 10.2514/1.A35434
收录情况：SCIE、EI -
Design of multistage compression waverider based on the local-turning osculating cones method
Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics,0459-1879,2022-03-18.
Zheng, Xiaogang (1); Zhu, Chengxiang (1); You, Yancheng (1)
EI:20221511958488 10.6052/0459-1879-21-357
收录情况：EI -
Local-Turning Osculating Cones Method for Waverider Design
AIAA JOURNAL,0001-1452,2020-08.
Zheng, Xiaogang; Hu, Zhancang; Li, Yiqing; Zhu, Chengxiang; You, Yancheng; Song, Wenjia
WOS:000560023000021 10.2514/1.J059139
收录情况：SCIE
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考虑巡航攻角的三维内转进气道设计与分析
航空学报,1000-6893,2024-12-02.
郑晓刚;胡占仓;蔡泽君;施崇广;朱呈祥;尤延铖
CSCD核心库 -
高超声速三维内转进气道研究进展综述
航空学报,1000-6893,2024-12-02.
郑晓刚;施崇广;张加乐;张咪;朱文磊;朱呈祥;尤延铖
CSCD核心库 -
三维弯曲流面法及其在外流乘波体中的应用
航空学报,1000-6893,2024-06-19.
杨凯;张勐飞;施崇广;余耀堃;郑晓刚;朱呈祥;尤延铖
CSCD核心库 -
基于局部偏转吻切方法的背部进气高超飞行器一体化设计研究
空天技术,2097-0714,2023-10-15.
郑晓刚;林德寿;方啸雷;尤延铖;朱呈祥
CSCD核心库 -
基于三维弯曲激波的宽域变马赫数乘波体设计分析
南京航空航天大学学报,1005-2615,2022-10-15.
尤延铖;郑晓刚;丁晓婷;汤祎麒;朱呈祥
CSCD核心 -
基于局部偏转吻切方法的多级压缩乘波体设计
力学学报,0459-1879,2022-03-18.
郑晓刚;朱呈祥;尤延铖
CSCD核心
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基于弯曲激波流场的内外流双乘波一体化设计及分析
推进技术,1001-4055,2025-03-20.
张勐飞;郑晓刚;汤祎麒;施崇广;尤延铖
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基于弯曲激波特征线法的两级压缩内收缩流场设计与分析
气体物理,2096-1642,2022-05-27.
汤祎麒;施崇广;郑晓刚;朱呈祥;尤延铖
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基于弯曲激波特征线法的两级压缩内收缩流场设计与分析
气体物理,2096-1642,2022-05-27.
汤祎麒;施崇广;郑晓刚;朱呈祥;尤延铖